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NACA-TR-D-1201

Performance and boundary-layer data from 12 degree and 23 degree conical diffusers of area ratio 2.0 at Mach numbers up to choking and Reynolds numbers up to 7.5 x 10(6)

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1954

Abstract: For each of two inlet-boundary-layer thicknesses, performance and boundary-layer characteristics have been determined for a 12 degree, 10-inch-inlet-diameter diffuser, a 12 degree, 21-inch-inlet-diameter diffuser, and a 23 degree, 21-inch-inlet-diameter diffuser. The investigation covered an inlet Mach number range from about 0.10 to coking. The corresponding inlet Reynolds number, based on inlet diameter, varied from about 0.5 x 10(6) to 7.5 x 10(6).
URI: https://yse.yabesh.ir/std/handle/yse/75961
Subject: AIR INTAKES
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    NACA-TR-D-1201

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:12:42Z
date available2017-09-04T16:12:42Z
date copyright01/01/1954
date issued1954
identifier otherSPONEEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/75961
description abstractFor each of two inlet-boundary-layer thicknesses, performance and boundary-layer characteristics have been determined for a 12 degree, 10-inch-inlet-diameter diffuser, a 12 degree, 21-inch-inlet-diameter diffuser, and a 23 degree, 21-inch-inlet-diameter diffuser. The investigation covered an inlet Mach number range from about 0.10 to coking. The corresponding inlet Reynolds number, based on inlet diameter, varied from about 0.5 x 10(6) to 7.5 x 10(6).
languageEnglish
titleNACA-TR-D-1201num
titlePerformance and boundary-layer data from 12 degree and 23 degree conical diffusers of area ratio 2.0 at Mach numbers up to choking and Reynolds numbers up to 7.5 x 10(6)en
typestandard
page24
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1954
contenttypefulltext
subject keywordsAIR INTAKES
subject keywordsANALYSIS (MATHEMATICS)
subject keywordsBOUNDARY LAYERS
subject keywordsCONICAL INLETS
subject keywordsDIFFUSERS
subject keywordsDISPLACEMENT
subject keywordsGROWTH
subject keywordsPRESSURE DISTRIBUTION
subject keywordsPRESSURE DROP
subject keywordsTHICKNESS
subject keywordsVELOCITY DISTRIBUTION
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